Method of driving rotation of a rotorcraft rotor by anticipating torque needs between two rotary speed setpoints of the rotor
AssigneeAirbus Helicopters
InventorsJean-Baptiste VALLART, Hilario VIEIRA
Life of this patent
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AssigneeAirbus Helicopters
InventorsJean-Baptiste VALLART, Hilario VIEIRA
Estimating the term…
A method of driving a rotorcraft rotor (1, 2) at variable controlled speeds. Starting from a required speed (Nr), a setpoint for total power (Pt) is calculated while taking account of an anticipated power (Pf) to be delivered by the power plant (3) for driving the main rotor (1) at the required speed (Nr), and while taking account of a power surplus (S) relating to progressive power needs to be delivered from a current power (Pc) for driving the main rotor (1) at a current speed (V) of rotation to an anticipated power (Pf) for driving the main rotor (1) at the required speed (Nr). By way of example, account may be taken at least of the acceleration or conversely of the deceleration of the main rotor (1) between the current speed (V) and the required speed (Nr), or indeed account may be taken of the flight circumstance of the rotorcraft 30 determining the calculated required speed (Nr).
A method of driving rotation of at least one rotorcraft rotor by a power plant of the rotorcraft, the method comprising the following operations:
A method of driving rotation of at least one rotorcraft rotor by a power plant of the rotorcraft, the method comprising the following operations:
A rotorcraft comprising:
Dependencies are inferred from the claim text.